Experimental cross-flow control in a 3D boundary layer by multi-discharge plasma actuators
| Autor: | Sergey L. Chernyshev, V. A. Yamshchikov, Dmitry S. Sboev, Stepan Tolkachev, I. E. Rebrov, Andrey Ph. Kiselev, S. I. Moshkunov, Vladislav Yu. Khomich, Sergey Baranov, Aleksandr P. Kuryachii |
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| Rok vydání: | 2021 |
| Předmět: |
0209 industrial biotechnology
Materials science Aerospace Engineering 02 engineering and technology Aerodynamics Dielectric barrier discharge Mechanics 01 natural sciences 010305 fluids & plasmas Vortex Boundary layer Flow control (fluid) 020901 industrial engineering & automation 0103 physical sciences Plasma actuator Pressure gradient Wind tunnel |
| Zdroj: | Aerospace Science and Technology. 112:106643 |
| ISSN: | 1270-9638 |
| Popis: | In this work, we perform experimental studies on the electrophysical and aerodynamic characteristics of two multi-discharge actuator models using near-surface dielectric barrier discharge to generate a unidirectional volumetric force impact over an extended surface area. Flow control experiments are conducted on the 3D boundary layer of a swept plate with an induced longitudinal pressure gradient using the aforementioned models in a subsonic low-turbulence wind tunnel. The results confirm the possibility of significantly decreasing the cross flow velocity in the boundary layer and stationary vortex intensity attenuation of its instability, owing to the extended volumetric force impact generated by the multi-discharge actuator system. |
| Databáze: | OpenAIRE |
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